System for the placement of modular fill material forming co-joined assemblies

ABSTRACT

A system for the placement of modular fill material forming co-joined assemblies that promotes increased efficiency in fill material building methods by utilizing the capabilities of aerial conveyance devices, the pre-assembly of forms, the rapid bracing of forms, and the sequential placement of enclosure forms.

BACKGROUND OF THE INVENTION

[0001] Generally, this invention relates to a system for creatinghardened structural forms made out of a fill material such as concrete.Specifically, the invention includes methods and apparatus for placingforming structures that are used to create such hardened forms. Theinvention is particularly suited for aerial transportation of formingstructures to create high-rise building structures.

[0002] The use of insulating concrete forms to create concrete buildingstructures increasingly is becoming a popular choice for building in theconstruction industry. Using insulating concrete forms as a buildingmethod typically involves placing a concrete form having a hollowinterior into which concrete can be poured. Upon hardening, the concreteprovides a hardened form that can be used as a component of a buildingstructure, for example, a wall. In the case of insulating concreteforms, the form itself may be made out of an insulating material or havean insulating material attached. After the concrete hardens, theinsulating material can be left in place, resulting in a hardenedstructure with both the building properties of concrete and theinsulating properties of the form.

[0003] When compared to traditional building methods, such as woodframing, the use of insulating concrete forms offers many attractiveadvantages. Building structures made out of concrete typically are moredurable and long-lasting than their non-concrete counterparts. This canbe an important consideration in areas prone to natural events such ashurricanes or earthquakes. Concrete building structures also may requirea reduced time and cost for maintenance than building structures madeusing other types of building methods. In the case of insulatingconcrete forms, the insulating properties of the form add furtherbenefits such as increased energy efficiency and noise reduction withinthe interior of the building structure. Further, the popularity of thiskind of building method may only increase as advances are made in thestate of the art. For example, concrete may no longer be the fillmaterial of choice as other kinds of fill materials are explored, andinsulating forms may no longer be required as other methods ofinsulation may be developed.

[0004] Despite these advantages, building with fill materials stillentails significant problems related to efficiency andcost-effectiveness that largely have not been overcome. One problemposed by conventional fill material building methods relates to themethod of placing forms. Many techniques still rely on manual labor toindividually place forms one at a time. This entails significantdrawbacks including large work crews required to perform thislabor-intensive task and extended periods of time in which to accomplishplacement of the forms. Certain improvements over manual labortechniques have been realized in the field. For example, the use of acrane to place forms has been described in U.S. Pat. No. 6,530,553, aswell as in various industry publications and proprietary websites. Whilethe use of a crane does reduce the size of the work crew needed andincreases the rate at which forms may be placed, it is somewhatremarkable that none of the foregoing applications has realized the fullpotential to which a crane may be used. For example, U.S. Pat. No.6,530,553 is limited to the use of a crane to place interior room formswithin a pre-established outside perimeter wall form. This type oftechnique relies on using forms fabricated into shapes andconfigurations for use on a particular job and overlooks the benefit ofusing standardized forms that can be assembled into a variety ofconfigurations. However, even techniques using standardized forms havefailed to appreciate the full capabilities of using a crane. Forexample, some industry publications and websites merely disclose using acrane to transport a pallet of forms to a site of assembly. While thisreduces some of the labor and time costs associated with placing formsby increasing the efficiency of transporting forms to an assembly site,manual labor with all of its drawbacks may be still required to placethe forms at the assembly site. Finally, even techniques in which acrane is used to place a form have until now failed to fully understandthe potential to which a crane may be used. For example, someproprietary websites actually illustrate a form connected to a cranewith a caption stating that the particular crane advertised is ideal forhandling gang forms. Nevertheless, no disclosure is made of a joinedform connected to a crane. This collection of seemingly unattached formsis then moved to a placement location.

[0005] Another problem posed by conventional fill material buildingmethods relates to the pre-assembly of forms. Building methods involvingfill materials frequently call for placing metal reinforcement bars, orrebar, within a form to strengthen the final hardened form. Manytechniques for placing rebar require using manual labor at aninstallation location. Again, this may entail significant drawbacks,perhaps including large work crews required to perform thislabor-intensive task and extended periods of time in which to accomplishplacement of the rebar. This technique may fail to appreciate the valueof preloading rebar into a form and placing the form at an installationlocation with rebar already loaded. However, while certain industrypublications and propriety websites acknowledge the value of preloadingrebar, even these sources fail to fully appreciate the full benefit ofhow this may be accomplished. For example, certain proprietary websitesillustrate a crane lifting a pallet of forms with loaded rebar to alocation for placement at an assembly site. Again, however, this methodrequires manual labor with all of its associated drawbacks to place theforms once they reach the assembly site.

[0006] A further problem relates to placing forms on high-risestructures. Construction techniques for building high-rise structuresfrequently employ cranes, and some industry publications and proprietarywebsites indicate the use of a crane to lift forms to a high-riselocation or perhaps more than one story above the ground. However, eventhese sources may to some degree fail to fully appreciate the degree towhich one might be able to increase the efficiency of high-riseconstruction. Consequently, these techniques have failed to fullyappreciate the usefulness of a crane in fill material building methodsat high-rise locations.

[0007] Yet another problem relates to bracing forms that have beenplaced. Typically, a placed form requires bracing to hold it in placeagainst, for example, wind loads that may develop on the cross-sectionalarea of a placed form. One typical method for bracing a placed forminvolves the use of a kicker. However, positioning a kicker so that itis properly aligned to the form and so that the form is properly plumbfrequently entails a time-intensive manual procedure. This procedure mayfurther be complicated by the necessity of solidly securing the kickerto the form. While the time required to accomplish this for anindividual kicker may not be significant, a typical construction jobwill require many kickers to be placed. This may cause the total timerequired to position kickers to become a significant expense. Existingmethods of positioning kickers may not promote efficiency inaccomplishing this task. For example, U.S. Pat. No. 4,068,427 requires atrack to be installed on a form to which a kicker may be connected. U.S.Pat. No. 4,068,427 further does not allow the kicker to be placedagainst the form in a continuously adjustable manner. These techniquesfail to appreciate the efficiency of connecting a kicker directly to aform.

[0008] An additional problem relates to methods for placing forms incorner locations and other locations that may need to be enclosed. Manytechniques do not accommodate special conditions for corners of thelike. For example, building methods involving fill material formsfrequently require an opening between two forms to be closed. Generally,this can involve placing rebar into the opening, connecting to the rebarof the adjoining forms, and closing the opening with an inner panel andan outer panel. It may normally be the case that the rebar may be placedfirst and the form subsequently closed with an inner panel and an outerpanel. However, high-rise building methods can present specialcircumstances. Specifically, it may be the case that an exterior walllocated more than one story above the ground may be practically accessedonly from the interior of the building. Many conventional systems mayeven require simultaneous placement of both the inner panel and theouter panel, which may limit the opportunity to place rebar into a spacebetween the forms. Consequently, conventional building systems may failto accommodate this aspect of high-rise construction.

[0009] One more problem may relate to further techniques for bracingforms. Many techniques do not accommodate special conditions in whichthe placement location of a brace may be important. For example, inhigh-rise construction, it may not be practical to place a brace on theexterior side of an exterior wall located more than one story above theground. Consequently, conventional techniques that require a brace to beplaced on both sides of a form may have limited application in high-risebuilding construction.

[0010] The foregoing problems regarding fill material building methodsmay represent a long-felt need for an effective solution. Whileimplementing elements may have been available, actual attempts to meetthis need may have been lacking to some degree. This may have been dueto a failure of those having ordinary skill in the art to fullyappreciate or understand the nature of the problems and challengesinvolved. As a result of this lack of understanding, attempts to meetthese long-felt needs may have failed to effectively solve one or moreof the problems or challenges here identified. These attempts may evenhave led away from the technical directions taken by the presentinvention and may even result in the achievements of the presentinvention being considered to some degree an unexpected result of theapproach taken by some in the field.

SUMMARY OF THE INVENTION

[0011] Accordingly, the present invention provides a system for theplacement of modular fill material forming co-joined assemblies. Someembodiments of the invention may include placing specialized modularfill material forming co-joined assemblies through the use of an aerialconveyance device such as a crane. Other embodiments of the inventionmay involve pre-assembling specialized forms for use with an aerialconveyance device. Further embodiments of the invention may includemethods and apparatus for bracing forms that have been placed. Stillfurther embodiments of the invention may involve methods and apparatusfor closing corners and other types of openings formed between modularfill material forming co-joined assemblies. Some embodiments of theinvention may involve placing and bracing pre-assembled specializedmodular fill material forming co-joined assemblies with an aerialconveyance device and closing corners and other types of openings formedbetween such structures after they are placed and braced. Certainembodiments of the invention may be particularly useful for high-riseconstruction projects. It may be the case that embodiments of thecurrent invention may increase the time and cost efficiencies ofbuilding methods that utilize fill material forms.

[0012] A significant object of the invention may be to increase the timeand cost efficiencies of placing fill material forms.

[0013] In keeping with this object, it may be a goal of the invention toincrease the effectiveness of using an aerial conveyance device such asa crane to place fill material forms.

[0014] In further keeping with this object, it may be a goal of theinvention to increase the effectiveness of using pre-assembled fillmaterial forms with an aerial conveyance device such as a crane.

[0015] In further keeping with this object, it may be a goal of theinvention to increase the effectiveness of bracing forms that have beenplaced using an aerial conveyance device such as a crane.

[0016] In further keeping with this object, it may be a goal of theinvention to increase the effectiveness of closing corners and othertypes of openings that may be part of the process of using buildingmethods involving fill material forms.

[0017] In further keeping with this object, it may be a goal of theinvention to facilitate the use of fill material building methods inhigh-rise construction projects.

[0018] Naturally, further objects and goals of the invention will becomeapparent from the description and drawings below.

BRIEF DESCRIPTION OF THE DRAWINGS

[0019]FIG. 1 shows a perspective view of two fill material forms.

[0020]FIG. 2 shows a perspective view of two fill material forms joinedto create a modular fill material forming co-joined assembly.

[0021]FIG. 3 shows a perspective view of a modular fill material formingco-joined assembly attached to an aerial conveyance device.

[0022]FIG. 4 shows a perspective view of a modular fill material formingco-joined assembly being placed while connected to an aerial conveyancedevice.

[0023]FIG. 5 shows a plan view of a brace attachment element joined to amodular fill material forming co-joined assembly.

[0024]FIG. 6 shows a sectional view of a brace attachment element joinedto a modular fill material forming co-joined assembly.

[0025]FIG. 7 shows a perspective view of two enclosure locations formedbetween placed modular fill material forming co-joined assemblies.

[0026]FIG. 8 shows a perspective view of two outer enclosure formingpanels placed at two enclosure locations.

[0027]FIG. 9 shows a perspective view of two enclosure reinforcementmembers placed at two enclosure spaces.

[0028]FIG. 10 shows a perspective view of two inner enclosure formingpanels placed between two modular fill material forming co-joinedassemblies.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0029] As mentioned earlier, the present invention includes a variety ofaspects, which may be combined in different ways. The followingdescriptions are provided to list elements and describe some of theembodiments of the present invention. These elements are listed withinitial embodiments, however it should be understood that they may becombined in any manner and in any number to create additionalembodiments. The variously described examples and preferred embodimentsshould not be construed to limit the present invention to only theexplicitly described systems, techniques, and applications. Further,this description should further be understood to support and encompassdescriptions and claims of all the various embodiments, systems,techniques, methods, devices, and applications with any number of thedisclosed elements, with each element alone, and also with any and allvarious permutations and combinations of all elements. Accordingly,methods and apparatus are disclosed for the placement of modular fillmaterial forming co-joined assemblies in certain embodiments of theinvention.

[0030] Referring now primarily to FIG. 1, in some embodiments of theinvention, a first forming panel (1) and a second forming panel (2) maybe arranged in substantially opposed parallel orientation. A formingpanel may be an object capable of forming a fill material into a shapedefined at least in part by the physical definition of the formingpanel. A forming panel may have a substantially planar surface or mayhave a non-planar surface, which may include a curved surface. Aparallel orientation into which forming panels may be arranged mayinclude forming panels arranged so as to be substantially equidistantfrom one another. Configurations into which forming panels aresubstantially equidistant to one another may include equidistant lines,equidistant curves, equidistant flat planes, equidistant curved planes,and concentric spherical surfaces or portions thereof. An opposedorientation into which forming panels may be arranged may include panelsplaced so as to be opposite to one another. It may readily beappreciated by those skilled in the art that the dimensions of a panelmay vary depending on the specific application for which the panel maybe used, including panels which may have a vertical axis longer than ahorizontal axis and panels which may have a horizontal axis longer thana vertical axis. It also may be appreciated by those skilled in the artthat a panel may include openings within the panel, including forexample but not limited to window openings or door openings.

[0031] In certain applications, a forming panel may be an insulatingforming panel. An insulating forming panel may be a forming panel havinginsulating properties, which under some circumstances may include aforming panel made out of an insulting material. Such insulatingmaterials may include expanded polystyrene or extruded polystyrene, ormay include other materials typically used in the construction industryto impart insulating properties to a building structure. In otherapplications, the materials out of which a forming panel may be made maybe selected without regard to insulating properties. Such materials mayinclude wood, fiber, polymer, steel, metal alloy, epoxy, or plasticcomposite.

[0032] Certain embodiments of the invention may include a first formingpanel (1) and a second forming panel (2) that may be arranged to form aspace (3). The space (3) may exist between a first forming panel (1) anda second forming panel (2) arranged in substantially opposed parallelorientation. The width of the space (3) may be varied depending on theapplication for which the panels are to be used. In some applications,this may include pouring a fill material into a space (3) of a fillmaterial forming panel (9).

[0033] A first forming panel (1) and a second forming panel (2) may incertain embodiments of the invention be joined by a connection element(4). A connection element (4) may be an element that is joined to bothfirst forming panel (1) and second forming panel (2).

[0034] In some applications, a connection element (4) may be a rigid tie(5). This may be merely a tie that is substantially rigid, such as a tiethat maintains its shape in the course of conditions usuallyencountered. The rigid tie (5) also may maintain a separation distancebetween a first forming panel (1) and a second forming panel (2). Such arigid tie may be established as a rigid separation distance maintenanceelement. Maintenance of a separation distance may include preserving thewidth of space (3) between a first forming panel (1) and a secondforming panel (2).

[0035] In other applications, a connection element (4) may be a flexibletie (8). This may be merely a tie that is substantially flexible, suchas a tie that is substantially deformable in the course of conditionsusually encountered. Under some circumstances, a connection element thatis substantially deformable may include a folding tie, a pivot tie, anelastic tie, a wire tie, a monofilament tie, a frictional surface tie,or a flexible mesh tie. A folding tie may be a tie having a portioncapable bending over upon itself. A pivot tie may be a tie having apoint about which two or more portions of the tie may rotate. An elastictie may be a tie capable of returning to its original configurationafter being stretched, compressed, expanded, or otherwise deformed. Awire tie may be a tie configured as a cord, cable, or related structure.A monofilament tie may be a tie made of a single fibrous element. Africtional surface tie may be a tie in which two surfaces are joined atan interface that is resistive to motion. A flexible mesh tie may be atie made of a substantially flexible network of interwoven orinterlinked elements.

[0036] A flexible tie (8) also may maintain a separation distancebetween a first forming panel (1) and a second forming panel (2). Such aflexible tie may be established as a flexible separation distancemaintenance element. Maintenance of a separation distance may includepreserving the width of space (3) between a first forming panel (1) anda second forming panel (2). Preservation of the width of space (3) mayinclude holding a first forming panel (1) and a second forming panel (2)in place so as to prevent first forming panel (1) or second formingpanel (2) from falling out of position and changing the width of space(3).

[0037] In some embodiments of the invention, a flexible tie (8) also maybe adapted to permit a first forming panel (1) to be collapsed withrespect to second forming panel (2). Collapsing a first forming panel(1) and a second forming panel (2) may include bringing a first formingpanel (1) and a second forming panel (2) into substantial contact so asto substantially eliminate space (3) between a first forming panel (1)and a second forming panel (2). Adapting a flexible tie (8) to allow fora first forming panel (1) and a second forming panel (2) to be collapsedmay include substantially deforming flexible tie (8) so as to bring afirst forming panel (1) and a second forming panel (2) into substantialcontact.

[0038] In other embodiments of the invention, a connection element (4)may be an adjustable tie. An adjustable tie may be a tie the length ofwhich may be adjusted in order to vary the width of space (3) formedbetween a first forming panel (1) and a second forming panel (2). Anadjustable tie may be a crimp-adjustable tie. A crimp-adjustable tie maybe a tie the length of which may be adjusted by crimping or perhapsdeforming some area or perhaps even a portion of the length of a tie.Crimping at least a portion of the length of a tie may include pinchingat least one fold into at least a portion of the length of a tie,although many other arrangements are possible.

[0039] In certain embodiments of the invention, a reinforcement member(6) may be placed within space (3). A reinforcement member (6) may be amember intended to be embedded within a hardened form that may evenconfer strength to a hardened form. In some applications, areinforcement member (6) may be a metal reinforcement bar, or perhapsrebar. A reinforcement member (6) may be placed within space (3) byhorizontally or vertically inserting reinforcement member (6) into space(3). A reinforcement member (6) also may be placed in a horizontalorientation or a vertical orientation. A horizontal orientation ofreinforcement member (6) may be an orientation parallel to a top side oran under side of space (3) formed by a first forming panel (1) and asecond forming panel (2). A vertical orientation may be an orientationparallel to a left side or a right side of space (3) formed by a firstforming panel (1) and a second forming panel (2). A reinforcement member(6) also may be placed within a space (3) at a remote location, at aground location, or at a placement location. It also may be that areinforcement member (6) is placed within a space (3) before a modularconcrete forming structure (10) is lifted. This may be because placing areinforcement member (6) within a space (3) before a modular fillmaterial forming co-joined assembly (10) is lifted may reduce theincreased time, effort, and difficulty that may result from placing areinforcement member (6) within a space (3) at a location of a modularfill material forming co-joined assembly (10) after a modular fillmaterial forming co-joined assembly (10) is lifted.

[0040] Under some circumstances, a rigid tie (5) also may be adapted tobe joined to a reinforcement member (6). Adapting rigid tie (5) to bejoined to reinforcement member (6) may include fabricating rigid tie (5)to receive a reinforcement member (6). A rigid tie (5) may be fabricatedto include a cradle (7). A cradle (7) may be a shape of rigid tie (5)adapted to receive and hold in place to some degree a reinforcementmember (6).

[0041] Under other circumstances, a flexible tie (8) may be adapted tobe joined to a reinforcement member (6). Adapting flexible tie (8) to bejoined to reinforcement member (6) may include spreading a flexible tie(8) to place flexible tie (8) under tension. Spreading flexible tie (8)may be accomplished by increasing the width of space (3) between a firstforming panel (1) and a second forming panel (2) to which flexible tie(8) may be connected. A tension experienced by spreading flexible tie(8) may allow flexible tie (8) to acquire a degree of stiffness. Adegree of stiffness acquired by flexible tie (8) may provide sufficientsupport to join a reinforcement member (6) to flexible tie (8).

[0042] In may also be that a reinforcement member (6) may be joined toconnection element (4). Joining reinforcement element (6) to connectionelement (4) may include tying down reinforcement element (6) toconnection element (4).

[0043] In some embodiments of the invention, a fill material form (9)may be established by having at least a first forming panel (1) and asecond forming panel (2) arranged in substantially opposed parallelorientation with a space (3) between a first forming panel (1) and asecond forming panel (2) and a connection element (4) joined to at leasta first forming panel (1) and a second forming panel (2). It further maybe understood by those skilled in the art that a first forming panel (1)and a second forming panel (2) may further themselves be formed byjoining together a number of sub-panels.

[0044] Referring now primarily to FIG. 2, in some embodiments of theinvention, at least two fill material forms may be joined to create amodular fill material forming co-joined assembly (10). In someapplications, a modular fill material forming co-joined assembly (10)may be joined at a remote location. A remote location may be a locationthat is distant from a ground location and a placement location, perhapseven a factory site. A factory site may be a site at which formingpanels and fill material forms are fabricated. A modular fill materialforming co-joined assembly (10) joined at a remote location further maybe transported from a remote location to a ground location. A groundlocation may be a location at a building structure site of a modularfill material forming co-joined assembly (10) prior to lifting a modularfill material forming co-joined assembly (10) and transporting a modularfill material forming co-joined assembly (10) to a placement location. Abuilding structure site may be a site at which a building structure isconstructed. Under some circumstances, a modular fill material formingco-joined assembly (10) also may be joined at a ground location, perhapsat the building structure site.

[0045] Referring again primarily to FIG. 1, In certain embodiments ofthe invention, a first fill material form (11) may have a first edge(12) and a second edge (13), and a second fill material form (14) mayhave a third edge (15) and a fourth edge (16). In some applications, afirst fill material form (11) may be joined to a second fill materialform (14) by joining a first rail (17) to a first edge (12) and a thirdedge (15). In other applications, a first fill material form (11) may bejoined to a second fill material form (14) by joining a second rail (18)to a second edge (13) and a fourth edge (16). In other situations, afirst fill material form (11) may be joined to a second fill materialform (14) in the manner described by substituting a first clip for saidfirst rail (17) and a second clip for said second rail (18). It furtherwill be appreciated by those skilled in the art that any manner ofsuitable fastener or connection element may be used to join a first fillmaterial form (11) and a second fill material form (14).

[0046] Referring again primarily to FIG. 2, certain embodiments of theinvention may permit a first fill material form (11) to be joined to asecond fill material form (14) to create a cavity (19) of a modular fillmaterial forming co-joined assembly (10) defined by communication ofeach said space (3) of a first fill material form (11) and a second fillmaterial form (14).

[0047] Now referring primarily to FIG. 3, in some embodiments of theinvention, a lift securement element (20) may be established on amodular fill material forming co-joined assembly (10). A lift securementelement (20) may be an element to which a lift attachment element (22)may be connected without structural or other damage to the modular fillmaterial forming co-joined assembly (10). In some applications, a liftsecurement element (20) may be a hook, clasp, ring, frictional surface,weld, tie, strap, mechanical fastener, or connector.

[0048] In other applications, a lift securement element (20) may be areinforcement member (6). A reinforcement member (6) may be placed in aspace (3) in a horizontal orientation or a vertical orientation. A liftsecurement element (20) that may be a reinforcement element (6) mayfurther be adapted for connection to a lift attachment element (22).Adapting a reinforcement member (6) for connection to a lift attachmentelement (22) may include forming a shape of reinforcement element (6)that facilitates connection of reinforcement element (6) to liftattachment element (22).

[0049] Certain embodiments of the invention may include establishing anaerial conveyance device (21). An aerial conveyance device (21) may be acrane, an elevator, a lift, a pulley system, an aircraft, or a liftingsystem. It may be that a lift attachment element (22) may be establishedon an aerial conveyance device (21). A lift attachment element (22) maybe an element that may connect to lift securement element (20). In someapplications, a lift attachment element (22) may be a hook, clasp,crimp, ring, tong, frictional surface, weld, tie, strap, mechanicalfastener, or connector. In other applications, a lift attachment element(22) may further be adapted for connection to a lift securement element(20) that is a reinforcement member (6). Adapting a lift attachmentelement (22) for connection to a reinforcement member (6) may includeforming a shape of lift attachment element (22) that facilitatesconnection of lift attachment element (22) to reinforcement member (6).

[0050] In some embodiments of the invention, a securement integritysystem may be established on a modular fill material forming co-joinedassembly. A securement integrity system may be a system to fortify astructural integrity of a modular fill material forming co-joinedassembly (10) during lifting or transporting of a modular fill materialforming co-joined assembly (10). Fortification of structural integritymay include strengthening structural integrity to enable a modular fillmaterial forming co-joined assembly to better withstand stresses thatmay be induced by lifting and transporting, especially if loaded withrebar. Accordingly, at least one strengthening element may beestablished on a modular fill material forming co-joined assembly (10).A strengthening element may be an element that imparts adequate orperhaps merely increased strength to the structural integrity of amodular fill material forming co-joined assembly (10). Under somecircumstances, a strengthening element may be a high-strength fastenerjoining a lift securement element (20) to a component of a modular fillmaterial forming co-joined assembly (10).

[0051] Of course, a modular fill material forming co-joined assembly(10) may have a centroid (45). Under some circumstances, it may be thata centroid (45) of a modular fill material forming co-joined assembly(10) may be estimated prior to positioning a lift securement element(20). In some applications, a centroid (45) of a modular fill materialforming co-joined assembly (10) may be a mass centroid (45) or an areacentroid (45). A centroid (45) of a modular fill material formingco-joined assembly (10) may further have an axis of lift. An axis oflift for a centroid (45) of a modular fill material forming co-joinedassembly (10) may be an axis oriented in the direction in which amodular fill material forming co-joined assembly (10) may be lifted. Insome situations, an axis of lift for a centroid (45) of a modular fillmaterial forming co-joined assembly (10) may be an axis substantiallybetween a centroid (45) of a modular fill material forming co-joinedassembly (10) and the location of a lift securement element (20)established on a modular fill material forming co-joined assembly (10).In other situations, an axis of lift for a centroid (45) of a modularfill material forming co-joined assembly (10) may be an axissubstantially between a centroid (45) of a modular fill material formingco-joined assembly (10) and the location of a vector sum of the liftingvectors of more than one lift securement element (20).

[0052] It may be that at least one lift securement element (20) may bepositioned to correlate with the desired placement orientation, perhapsat least about a vertical axis, which may be an axis of lift for acentroid (45) of a modular fill material forming co-joined assembly(10). A position of a lift securement element (20) may be correlatedwith an axis of lift for a centroid (45) of a modular fill materialforming co-joined assembly (10) by being relationally responsive to anaxis of lift for a centroid (45) of a modular fill material formingco-joined assembly (10). Under some circumstances, it may be that atleast one lift securement element (20) may be relationally responsive toan axis of lift for a centroid (45) of a modular fill material formingco-joined assembly (10) by being symmetrically arranged about an axis oflift for a centroid (45) of a modular fill material forming co-joinedassembly (10). Such a lift securement element (20) may be established asa lift axis centroidally symmetric lift securement element.

[0053] In certain embodiments of the invention, a modular fill materialforming co-joined assembly (10) may be established at a ground location.A modular fill material forming co-joined assembly (10) at a groundlocation may have a ground orientation corresponding an orientation of amodular fill material forming co-joined assembly at a ground location. Aground orientation of the modular fill material forming co-joinedassembly (10) may be established to substantially coincide with anaerial orientation of a modular fill material forming co-joined assembly(10). An aerial orientation of a modular fill material forming co-joinedassembly (10) may correspond to an orientation of a modular fillmaterial forming co-joined assembly (10) during transport of a modularfill material forming co-joined assembly (10) by an aerial conveyancedevice (21). A ground orientation that substantially coincides with anaerial orientation may be a ground orientation that is substantially thesame as an aerial orientation.

[0054] In some embodiments of the invention, a modular fill materialforming co-joined assembly (10) may be lifted from a ground location ofa modular fill material forming co-joined assembly (10). Lifting amodular fill material forming co-joined assembly (10) may includeremoving a modular fill material forming co-joined assembly (10) from aresting surface of a ground location. A modular fill material formingco-joined assembly (10) may be lifted in a direction of an axis of liftfor a centroid (45) of a modular fill material forming co-joinedassembly (10). Lifting of a modular fill material forming co-joinedassembly may be accomplished by connecting at least one lift securementelement (20) established on a modular fill material lifting structure(10) to at least one lift attachment element (22) of an aerialconveyance device (21) and using an aerial conveyance device (21) tolift a modular fill material forming co-joined assembly (10).

[0055] Now referring primarily to FIG. 4, in some embodiments of theinvention, a modular fill material forming co-joined assembly (10) maybe transported from a ground location of a modular fill material formingco-joined assembly (10) to a placement location of a modular fillmaterial forming co-joined assembly (10). A placement location of amodular fill material forming co-joined assembly (10) may be a locationat which a modular fill material forming co-joined assembly (10) isplaced for use. In some applications, a placement location of a modularfill material forming co-joined assembly (10) may include a fillmaterial pour site of a modular fill material forming co-joined assembly(10). A fill material pour site of a modular fill material formingco-joined assembly (10) may be a site at which fill material is pouredinto at least one space (3) of at least one fill material form (9) of amodular fill material forming co-joined assembly (10). It also may bethat a fill material pour site of a modular fill material formingco-joined assembly (10) may be a high-rise fill material pour site of amodular fill material forming co-joined assembly (10). A high-rise fillmaterial pour site of a modular fill material forming co-joined assembly(10) may be a pour site situated at a location that is at least onestory above the level of a ground location of a modular fill materialforming co-joined assembly (10).

[0056] Transporting a modular fill material forming co-joined assembly(10) may include transporting a modular fill material forming co-joinedassembly (10) in an aerial orientation while a lift securement element(20) established on a modular fill material forming co-joined assembly(10) is connected to a lift attachment element (22) of an aerialconveyance device (21). In some applications, an aerial orientation of amodular fill material forming co-joined assembly (10) may further beestablished or even adjusted to substantially coincide with a placementorientation of a modular fill material forming co-joined assembly (10)while a lift securement element (20) established on a modular fillmaterial forming co-joined assembly (10) is connected to a liftattachment element (22) of an aerial conveyance device (21). A placementorientation of a modular fill material forming co-joined assembly (10)may be an orientation at which a modular fill material placementstructure (10) is placed. An aerial orientation that substantiallycoincides with a placement orientation may be an aerial orientation thatis substantially the same as a placement orientation.

[0057] In certain embodiments of the invention, a modular fill materialforming co-joined assembly (10) may be placed at a placement location.Placing a modular fill material forming co-joined assembly (10) mayoccur when a modular fill material forming co-joined assembly (10) is ina placement orientation and while a lift securement element (20)established on a modular fill material forming co-joined assembly (10)is connected to a lift attachment element (22) of an aerial conveyancedevice (21). Placing a modular fill material forming co-joined assembly(10) may further include joining a modular fill material formingco-joined assembly (10) to at least one fill material form (9) at saidplacement location. A lift securement element (20) established on amodular fill material forming co-joined assembly (10) may bedisconnected from a lift attachment element (22) of an aerial conveyancedevice (21) after a modular fill material forming co-joined assembly(10) is placed.

[0058] Now referring primarily to FIG. 5 and FIG. 6, in some embodimentsof the invention, a brace attachment element (23) may be affixed to amodular fill material forming co-joined assembly (10). In someapplications, a brace attachment element (23) may be permanently joinedto a modular fill material forming co-joined assembly (10). In otherapplications, a brace attachment element (23) may be temporarily joinedto a modular fill material forming co-joined assembly (10).

[0059] In certain embodiments of the invention, a brace attachmentelement (23) may be affixed to a modular fill material forming co-joinedassembly (10) in a continuously repositionable location. A continuouslyrepositionable location may be a location the position of which may bemoved and perhaps secured in any incremental position without requiringmovement in discrete quantities. It may be that an exposed rail (24) maybe joined to a modular fill material forming co-joined assembly (10),and a brace attachment element (23) may be configured for a slideengagement of exposed rail (24). Such a brace attachment element (23)may be established as a slide engagement brace attachment element. Anopening may be established on brace attachment element (23), throughwhich a locking element (26) may be placed. A locking element (26)placed through an opening may act to lock brace attachment element (23)in a particular position to exposed rail (24). A locking element (26)may be a screw. A locking element (26) that is a screw may be aself-tapping screw. Under some circumstances, a brace attachment element(23) may be locked in place by a self-tapping screw that is embedded inexposed rail (24). A self-tapping screw may even penetrate through anexposed rail (24) and a first forming panel (1), embedding itself in asecond forming panel (2).

[0060] In some applications, a brace (27) may be attached to braceattachment element (23). A brace (27) may be a kicker (29). Under somecircumstances, a brace (27) may be attached to brace attachment element(23) through a pivot point (28). A brace (27) also may be anchored to ananchor location. In some embodiments of the invention it may be thatsubsequent to anchoring brace (27) at an anchor location, braceattachment element (23) may be continuously repositioned to a desiredlocation established on a modular fill material forming co-joinedassembly (10) and locked down at a desired location using lockingelement (26). A desired location may be a location at which a modularfill material forming co-joined assembly (10) may be in a plumbposition. It also may be that a brace (27) anchored to an anchorlocation and attached to brace attachment element (23) locked at adesired location may support a modular fill material forming co-joinedassembly (10).

[0061] In some embodiments of the invention, a brace attachment element(23) may be rapidly deployed. A deployment of brace attachment element(23) may include continuously repositioning brace attachment element(23) to a desired location and locking brace attachment element (23) inplace at a desired location. In some applications, a deployment mayinclude locking brace attachment (23) in place at a desired locationusing a screw. A rapid deployment of brace attachment element (23) mayinclude deploying brace attachment element (23) in a period of time thatmay be selected from the group consisting of about 90 seconds, about 2minutes, about 3 minutes, about 5 minutes, or about 10 minutes.

[0062] Now referring primarily to FIG. 7, it can be seen that anenclosure location (31) may be established. At least two fill materialforms (9) may be placed adjacent to enclosure location (31). Each fillmaterial form (9) may have an outer panel (41), an inner panel (42) anda space (3) formed between an outer panel (41) and an inner panel (42).A reinforcement member (6) may be placed within space (3) of each fillmaterial form (9).

[0063] In certain embodiments of the invention, an enclosure location(31) may be an in-line opening (32) established between at least twofill material forms (9) placed adjacent to an enclosure location (31).It may be readily understood by those skilled in the art that such anin-line opening may include an opening for a door, for a window, or foranother type of opening that may be necessary or desirable in aconstruction industry application. An in-line opening (32) establishedbetween at least two fill material forms (9) may have a width selectedfrom the group consisting of about 1 foot, about 2 feet, about 5 feet,or about 15 feet. In other embodiments of the invention, an enclosurelocation (31) may be a corner opening (33) established between at leasttwo fill material forms (9) placed adjacent to an enclosure location(31). It may be readily understood by those skilled in the art that sucha corner opening may include an opening for a door, for a window, or foranother type of opening that may be necessary or desirable in aconstruction industry application. A corner opening (33) establishedbetween at least two fill material forms (9) may have a width selectedfrom the group consisting of about 1 foot, about 2 feet, about 5 feet,or about 15 feet. An enclosure location (31) may be a fill material poursite. An enclosure location (31) that is a fill material pour site maybe a high-rise fill material pour site.

[0064] In some embodiments of the invention, an outer enclosure formingpanel (34), an inner enclosure forming panel (35), and an enclosurereinforcement member (36) may be transported to an enclosure location(31). An enclosure location (31) may have an outside enclosure boundary(37), an inside enclosure boundary (38), and an enclosure space (39). Anenclosure space (39) may be a space formed between an outside enclosureboundary (37) and an inside enclosure boundary (38). An outsideenclosure boundary (37) may be the boundary at which an outer enclosureforming panel (34) may need to be approximately positioned in order toenclose an enclosure location (31). In some applications, an outsideenclosure boundary may be configured to include two straight linesjoined at an angle. Under some circumstances, an outer enclosure formingpanel (34) may enclose an enclosure location (31) by being joined toeach outer panel of each adjacent fill material form (9). An insideenclosure boundary (38) may be the boundary at which an inner enclosureforming panel (35) may need to be positioned in order to enclose anenclosure location (31). In some applications, an inside enclosureboundary may be configured to include two straight lines joined at anangle. Under some circumstances, an inner enclosure forming panel (35)may enclose an enclosure location (31) by being joined to each innerpanel of each adjacent fill material form (9).

[0065] Now referring primarily to FIG. 8, in some embodiments of theinvention, an outer enclosure forming panel (34) may oriented tosubstantially coincide with an outside enclosure boundary (37) ofenclosure location (31). An orientation of outer enclosure forming panel(34) that substantially coincides with an outside corner boundary (37)may be an orientation of outer enclosure forming panel (34) that issubstantially the same as outside corner boundary (37). In somesituations, an outer enclosure forming panel (34) may then be positionedsubstantially at outside enclosure boundary (37). In other situations,an outer enclosure forming panel (34) may be positioned substantially atoutside enclosure boundary (37) after a modular fill material formingco-joined assembly (10) is placed on either side of enclosure location(31). In further situations, an outer enclosure forming panel (34) maybe positioned substantially at outside enclosure boundary (37) from aninside direction (43). An inside direction (43) may be that directioncorresponding to the side of enclosure location (31) at which innerenclosure forming panel (35) is placed and from which access withoutexterior support is necessary.

[0066] In some applications, a lift securement element (20) may beestablished on an outer enclosure forming panel (34). A lift securementelement (20) established on an outer enclosure forming panel (34) may beconnected to a lift attachment element (22) of an aerial conveyancedevice (21). An outer enclosure forming panel (34) which may then bepositioned substantially at outside enclosure boundary (37) may bepositioned while lift securement element (20) is connected to liftattachment element (22).

[0067] Now referring primarily to FIG. 9, in some embodiments of theinvention, an enclosure reinforcement member (36) may be oriented to fitwithin enclosure space (39). An enclosure reinforcement member (36) maythen be placed within enclosure space (39). Under some circumstances, anenclosure reinforcement member (36) may be placed within enclosure space(39) after an outer corner forming panel (34) may be positionedsubstantially at outside enclosure boundary (37). A lift securementelement (20) also may be established on an enclosure reinforcementmember (36). A lift securement element (20) established on an enclosurereinforcement member (36) may be connected to a lift attachment element(22) of an aerial conveyance device (21). An enclosure reinforcementmember (36) which may then be placed within an enclosure space (39) maybe placed while lift securement element (20) is connected to liftattachment element (22).

[0068] In certain embodiments of the invention, an enclosurereinforcement member (36) also may be joined to a reinforcement member(6) placed within space (3) of fill material form (9). An enclosurereinforcement member (36) joined to reinforcement member (6) may be tieddown (44) to reinforcement member (6). An enclosure reinforcement member(36) may be a metal reinforcement bar. In some situations, an enclosurereinforcement member (36) may be oriented with enclosure space (39) in ahorizontal orientation or a vertical orientation.

[0069] Now referring primarily to FIG. 10, in some embodiments of theinvention, an inner enclosure forming panel (35) may be oriented tosubstantially coincide with an inside enclosure boundary (38) ofenclosure location (31). An orientation of inner enclosure forming panel(35) that substantially coincides with an inside corner boundary (38)may be an orientation of inner enclosure forming panel (35) that issubstantially the same as inside corner boundary (38). In someapplications, an inner enclosure forming panel (35) may then bepositioned at inside enclosure boundary (38). In other applications, aninner enclosure forming panel (35) may be positioned substantially atinside enclosure boundary (38) after an enclosure reinforcement member(36) may be placed within enclosure space (39). A lift securementelement (20) also may be established on an inner enclosure forming panel(35). A lift securement element (20) established on an inner enclosureforming panel (35) may be connected to a lift attachment element (22) ofan aerial conveyance device (21). An inner enclosure forming panel (35)which may then be positioned substantially at inside enclosure boundary(38) may be positioned while lift securement element (20) is connectedto lift attachment element (22).

[0070] In some embodiments of the invention, an enclosure connectionelement may be joined to both an outer enclosure forming panel (34) andan inner enclosure forming panel (35). An enclosure connection elementmay be a connection element (4) utilized in a corner location (31). Insome applications, an outer enclosure forming panel (34) may besubstantially braced by inner enclosure forming panel (35). Outerenclosure forming panel (34) substantially braced by inner enclosureforming panel (35) may be braced substantially by the connection of anenclosure connection element to both outer enclosure forming panel (34)and inner enclosure forming panel (35).

[0071] Now referring to FIGS. 1-10, in some embodiments of theinvention, a fill material may be poured into at least one space (3) ofat least one fill material form (9) of a modular fill material formingco-joined assembly (10). A fill material may be a substantially fluidfill material capable of hardening into a hardened form. In someapplications, a fluid fill material capable of hardening into a hardenedform may be concrete. A fill material poured into at least one space (3)of at least one fill material form (9) of a modular fill materialforming co-joined assembly (10) may be molded into a shape defined by amodular fill material forming co-joined assembly. In some applications,a hardened form substantially made of a fill material may be a wall. Itmay be the case that a modular fill material forming co-joined assembly(10) may be removed from a hardened form after a fill material hashardened. A building structure may be created having a hardened form asat least one component. A building structure may include a building,tower, edifice, monument, or other residential, commercial or industrialstructure.

[0072] As can be easily understood from the foregoing, the basicconcepts of the present invention may be embodied in a variety of ways.It involves both modular fill material forming co-joined assemblyplacement techniques as well as devices to accomplish the appropriateplacement of modular fill material forming co-joined assemblies. In thisapplication, the modular fill material forming co-joined assemblyplacement techniques are disclosed as part of the results shown to beachieved by the various devices described and as steps which areinherent to utilization. They are simply the natural result of utilizingthe devices as intended and described. In addition, while some devicesare disclosed, it should be understood that these not only accomplishcertain methods but also can be varied in a number of ways. Importantly,as to all of the foregoing, all of these facets should be understood tobe encompassed by this disclosure.

[0073] The discussion included in this application is intended to serveas a basic description. The reader should be aware that the specificdiscussion may not explicitly describe all embodiments possible; manyalternatives are implicit. It also may not filly explain the genericnature of the invention and may not explicitly show how each feature orelement can actually be representative of a broader function or of agreat variety of alternative or equivalent elements. Again, these areimplicitly included in this disclosure. Where the invention is describedin device-oriented terminology, each element of the device implicitlyperforms a function.

[0074] It should also be understood that a variety of changes may bemade without departing from the essence of the invention. Such changesare also implicitly included in the description. They still fall withinthe scope of this invention. A broad disclosure encompassing both theexplicit embodiment(s) shown, the great variety of implicit alternativeembodiments, and the broad methods or processes and the like areencompassed by this disclosure. With this understanding, the readershould be aware that this disclosure is to be understood to support asbroad a base of claims as deemed within the applicant's right and apatent covering numerous aspects of the invention both independently andas an overall system.

[0075] Further, each of the various elements of the invention and claimsmay also be achieved in a variety of manners. Additionally, when used orimplied, an element is to be understood as encompassing individual aswell as plural structures that may or may not be physically connected.This disclosure should be understood to encompass each such variation,be it a variation of an embodiment of any apparatus embodiment, a methodor process embodiment, or even merely a variation of any element ofthese. Particularly, it should be understood that as the disclosurerelates to elements of the invention, the words for each element may beexpressed by equivalent apparatus terms or method terms—even if only thefunction or result is the same. Such equivalent, broader, or even moregeneric terms should be considered to be encompassed in the descriptionof each element or action. Such terms can be substituted where desiredto make explicit the implicitly broad coverage to which this inventionis entitled. As but one example, it should be understood that allactions may be expressed as a means for taking that action or as anelement that causes that action. Similarly, each physical elementdisclosed should be understood to encompass a disclosure of the actionthat that physical element facilitates. Regarding this last aspect, asbut one example, the disclosure of an “aerial conveyance device” shouldbe understood to encompass disclosure of the act of “aeriallyconveying”—whether explicitly discussed or not—and, conversely, werethere effectively disclosure of the act of “aerially conveying”, such adisclosure should be understood to encompass disclosure of an “aerialconveyance device” and even a “means for aerially conveying”. Suchchanges and alternative terms are to be understood to be explicitlyincluded in the description.

[0076] Any patents, publications, or other references mentioned in thisapplication for patent are hereby incorporated by reference. Inaddition, as to each term used it should be understood that unless itsutilization in this application is inconsistent with suchinterpretation, common dictionary definitions should be understood asincorporated for each term and all definitions, alternative terms, andsynonyms such as contained in the Random House Webster's UnabridgedDictionary, second edition are hereby incorporated by reference.Finally, all references listed in the list of References To BeIncorporated By Reference In Accordance With The Patent Application orother information statement filed with the application are herebyappended and hereby incorporated by reference, however, as to each ofthe above, to the extent that such information or statementsincorporated by reference might be considered inconsistent with thepatenting of this/these invention(s) such statements are expressly notto be considered as made by the applicant(s).

[0077] Thus, the applicant(s) should be understood to have support toclaim and make a statement of invention to at least: i) each of themodular fill material forming co-joined assembly devices as hereindisclosed and described, ii) the related methods disclosed anddescribed, iii) similar, equivalent, and even implicit variations ofeach of these devices and methods, iv) those alternative designs whichaccomplish each of the functions shown as are disclosed and described,v) those alternative designs and methods which accomplish each of thefunctions shown as are implicit to accomplish that which is disclosedand described, vi) each feature, component, and step shown as separateand independent inventions, vii) the applications enhanced by thevarious systems or components disclosed, viii) the resulting productsproduced by such systems or components, ix) each system, method, andelement shown or described as now applied to any specific field ordevices mentioned, x) methods and apparatuses substantially as describedhereinbefore and with reference to any of the accompanying examples, xi)the various combinations and permutations of each of the elementsdisclosed, and xii) each potentially dependent claim or concept as adependency on each and every one of the independent claims or conceptspresented.

[0078] With regard to claims whether now or later presented forexamination, it should be understood that for practical reasons and soas to avoid great expansion of the examination burden, the applicant mayat any time present only initial claims or perhaps only initial claimswith only initial dependencies. Support should be understood to exist tothe degree required under new matter laws—including but not limited toEuropean Patent Convention Article 123(2) and United States Patent Law35 USC 132 or other such laws—to permit the addition of any of thevarious dependencies or other elements presented under one independentclaim or concept as dependencies or elements under any other independentclaim or concept. In drafting any claims at any time whether in thisapplication or in any subsequent application, it should also beunderstood that the applicant has intended to capture as full and broada scope of coverage as legally available. To the extent thatinsubstantial substitutes are made, to the extent that the applicant didnot in fact draft any claim so as to literally encompass any particularembodiment, and to the extent otherwise applicable, the applicant shouldnot be understood to have in any way intended to or actuallyrelinquished such coverage as the applicant simply may not have beenable to anticipate all eventualities; one skilled in the art, should notbe reasonably expected to have drafted a claim that would have literallyencompassed such alternative embodiments.

[0079] Further, if or when used, the use of the transitional phrase“comprising” is used to maintain the “open-end” claims herein, accordingto traditional claim interpretation. Thus, unless the context requiresotherwise, it should be understood that the term “comprise” orvariations such as “comprises” or “comprising”, are intended to implythe inclusion of a stated element or step or group of elements or stepsbut not the exclusion of any other element or step or group of elementsor steps. Such terms should be interpreted in their most expansive formso as to afford the applicant the broadest coverage legally permissible.

[0080] Finally, any claims set forth at any time are hereby incorporatedby reference as part of this description of the invention, and theapplicant expressly reserves the right to use all of or a portion ofsuch incorporated content of such claims as additional description tosupport any of or all of the claims or any element or component thereof,and the applicant further expressly reserves the right to move anyportion of or all of the incorporated content of such claims or anyelement or component thereof from the description into the claims orvice-versa as necessary to define the matter for which protection issought by this application or by any subsequent continuation, division,or continuation-in-part application thereof, or to obtain any benefitof, reduction in fees pursuant to, or to comply with the patent laws,rules, or regulations of any country or treaty, and such contentincorporated by reference shall survive during the entire pendency ofthis application including any subsequent continuation, division, orcontinuation-in-part application thereof or any reissue or extensionthereon.

What is claimed is:
 1. A method of placing modular fill material forming co-joined assemblies, comprising the steps of: establishing at least two fill material forms, each said fill material form having at least a first forming panel and at least a second forming panel arranged in substantially opposed parallel orientation, a space formed between said at least first forming panel and said at least second forming panel, and at least one connection element joined to said first forming panel and said second forming panel; joining said at least two fill material forms to create a modular fill material forming co-joined assembly; establishing an outer enclosure forming panel, at least one enclosure reinforcement member, and an inner enclosure forming panel; establishing a ground location of said modular fill material forming co-joined assembly, said outer enclosure forming panel, said at least one enclosure reinforcement member, and said inner enclosure forming panel; establishing at least one lift securement element on said modular fill material forming co-joined assembly, said outer enclosure forming panel, said at least one enclosure reinforcement member, and said inner enclosure forming panel; establishing an aerial conveyance device having at least one lift attachment element; connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said modular fill material forming co-joined assembly; placing said modular fill material forming co-joined assembly in a placement location while said at least one lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said modular fill material forming co-joined assembly; disconnecting said at least one lift attachment element of said aerial conveyance device from said at least one lift securement element of said modular fill material forming co-joined assembly; affixing a brace attachment element joined to said modular fill material forming co-joined assembly in a continuously repositionable location; joining a brace to said brace attachment element; supporting said modular concrete forming structure with said brace; connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said outer enclosure forming panel; positioning said outer enclosure forming panel at an outside enclosure boundary of said enclosure location while said at least one lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said outer enclosure forming panel after said step of placing said modular fill material forming co-joined assembly; disconnecting said at least one lift attachment element of said aerial conveyance device from said at least one lift securement element of said outer enclosure forming panel; connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said enclosure reinforcement member; placing said enclosure reinforcement member within an enclosure space of said enclosure location while said at least one lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said outer enclosure forming panel after said step of positioning said outer enclosure forming panel; disconnecting said at least one lift attachment element of said aerial conveyance device from said at least one lift securement element of said enclosure reinforcement member; connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said inner enclosure forming panel; positioning said inner enclosure forming panel at an inner enclosure boundary of said enclosure location while said at least one lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said inner enclosure forming panel after said step of placing said enclosure reinforcement member; and disconnecting said at least one lift attachment element of said aerial conveyance device from said at least one lift securement element of said inner enclosure reinforcement panel.
 2. A method of placing modular fill material forming co-joined assemblies as described in claim 1, further comprising the step of placing at least one reinforcement member within said space of at least one said fill material form.
 3. A method of placing modular fill material forming co-joined assemblies as described in claim 2, wherein said reinforcement member comprises a steel reinforcement bar.
 4. A method of placing modular fill material forming co-joined assemblies as described in claim 2, wherein said step of placing said reinforcement member comprises the step of joining said reinforcement member to said connection element.
 5. A method of placing modular fill material forming co-joined assemblies as described in claim 2, wherein said step of placing said reinforcement member occurs before said step of placing said modular fill material forming co-joined assembly.
 6. A method of placing modular fill material forming co-joined assemblies as described in claim 1, wherein said connection element comprises a rigid tie.
 7. A method of placing modular fill material forming co-joined assemblies as described in claim 1, wherein said connection element comprises a flexible tie.
 8. A method of placing modular fill material forming co-joined assemblies as described in claim 7, wherein said flexible tie comprises a flexible tie adapted to permit at least one said fill material form to be collapsed.
 9. A method of placing modular fill material forming co-joined assemblies as described in claim 1, wherein said lift securement element comprises a lift securement element selected from the group consisting of a hook, clasp, ring, frictional surface, weld, tie, strap, mechanical fastener, or connector.
 10. A method of placing modular fill material forming co-joined assemblies as described in claim 1, wherein said lift securement element comprises a reinforcement member placed within at least one said space.
 11. A method of placing modular fill material forming co-joined assemblies as described in claim 1, wherein said aerial conveyance device comprises an aerial conveyance device selected from the group consisting of a crane, elevator, lift, pulley system, aircraft, or lifting system.
 12. A method of placing modular fill material forming co-joined assemblies as described in claim 1, wherein said lift attachment element comprises a lift attachment element selected from the group consisting of a hook, clasp, ring, tong, frictional surface, weld, tie, strap, mechanical fastener, or connector.
 13. A method of placing modular fill material forming co-joined assemblies as described in claim 1, further comprising the step of establishing a securement integrity system to fortify a structural integrity of said modular fill material forming co-joined assembly during said step of transporting said modular fill material forming co-joined assembly.
 14. A method of placing modular fill material forming co-joined assemblies as described in claim 1, further comprising joining at least one exposed rail to said modular fill material forming co-joined assembly.
 15. A method of placing modular fill material forming co-joined assemblies as described in claim 14, further comprising slidingly engaging said brace attachment element to said exposed rail.
 16. A method of placing modular fill material forming co-joined assemblies as described in claim 1, further comprising rapidly deploying said brace attachment element.
 17. A method of placing modular fill material forming co-joined assemblies as described in claim 16, wherein said step of rapidly deploying said brace attachment element comprises the step of deploying within a period of time selected from the group consisting of about 90 seconds, about 2 minutes, about 3 minutes, about 5 minutes, or about 10 minutes.
 18. A method of placing modular fill material forming co-joined assemblies as described in claim 1, further comprising joining said outer enclosure forming panel to an outer forming panel of said fill material form.
 19. A method of placing modular fill material forming co-joined assemblies as described in claim 1, further comprising joining said inner enclosure forming panel to an inner forming panel of said fill material form.
 20. A method of placing modular fill material forming co-joined assemblies as described in claim 2, further comprising joining said enclosure reinforcement member to said reinforcement member within said space of said fill material form.
 21. A method of placing modular fill material forming co-joined assemblies as described in claim 1, wherein said outer enclosure forming panel is substantially braced by said inner enclosure forming panel.
 22. A method of placing modular fill material forming co-joined assemblies as described in claim 21, further comprising the step of pouring a fill material into at least one said space after said step of placing said modular fill material forming co-joined assembly.
 23. A modular fill material forming co-joined assembly placement system, comprising: a first forming panel; a second forming panel; a fill material form having at least one connection element joined to at least said first forming panel and at least said second forming panel; a space within said fill material form between said first forming panel and said second forming panel; a modular fill material forming co-joined assembly having at least a first fill material form joined to at least a second fill material form; at least one lift securement element established on said modular fill material forming co-joined assembly; a brace attachment element affixed in a continuously repositionable location joined to said modular fill material forming co-joined assembly; a brace attached to said brace attachment element; an outer enclosure forming panel joined to said modular fill material forming co-joined assembly; an inner enclosure forming panel joined to said modular fill material forming co-joined assembly; and at least one enclosure reinforcing member placed with an enclosure spaced formed between said outer enclosure forming panel and said inner enclosure forming panel. 24-39. (Cancelled)
 40. A method of placing modular fill material forming co-joined assemblies, comprising the steps of: establishing at least two fill material forms, each said fill material form having at least a first forming panel and at least a second forming panel arranged in substantially opposed parallel orientation, a space formed between said at least first forming panel and said at least second forming panel, and at least one connection element joined to said first forming panel and said second forming panel; joining said at least two fill material forms to create a modular fill material forming co-joined assembly; establishing a ground location of said modular fill material forming co-joined assembly; establishing a ground orientation of said modular fill material forming co-joined assembly; estimating a centroid of said modular fill material forming co-joined assembly; establishing at least one lift securement element on said modular fill material forming co-joined assembly; positioning said at least one lift securement element to correlate with an axis of lift for said centroid of said modular fill material forming co-joined assembly; establishing an aerial conveyance device having at least one lift attachment element; connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said modular fill material forming co-joined assembly; lifting said modular fill material forming co-joined assembly in an aerial orientation along said axis of lift for said centroid using said aerial conveyance device; transporting said modular fill material forming co-joined assembly in said aerial orientation from said ground location to a placement location using said aerial conveyance device; establishing an aerial orientation of said modular fill material forming co-joined assembly to substantially coincide with said placement orientation of said modular fill material forming co-joined assembly while said at least one lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said modular fill material forming co-joined assembly; placing said modular fill material forming co-joined assembly oriented in said placement orientation in said placement location while said at least one lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said modular fill material forming co-joined assembly; and disconnecting said at least one lift attachment element of said aerial conveyance device from said at least one lift securement element of said modular fill material forming co-joined assembly.
 41. A method of placing modular fill material forming co-joined assemblies as described in claim 40, further comprising the step of placing at least one reinforcement member within said space of at least one said fill material form.
 42. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said reinforcement member comprises a steel reinforcement bar.
 43. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member occurs at a remote location.
 44. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member occurs at said ground location.
 45. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member occurs at said placement location.
 46. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member comprises the step of horizontally inserting said reinforcement member into said space of at least one said fill material form.
 47. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member comprises the step of vertically inserting said reinforcement member into said space of at least one said fill material form.
 48. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member comprises the step of placing said at least one reinforcement member in a horizontal orientation within said space of at least one said fill material form.
 49. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member comprises the step of placing said at least one reinforcement member in a vertical orientation within said space of at least one said fill material form.
 50. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said at least one reinforcement member comprises the step of joining said reinforcement member to at least one said connection element.
 51. A method of placing modular fill material forming co-joined assemblies as described in claim 50, wherein said step of joining said reinforcement member to at least one said connection element comprises the step of tying down said reinforcement member to said connection element.
 52. A method of placing modular fill material forming co-joined assemblies as described in claim 41, wherein said step of placing said reinforcement member occurs before said step of lifting said modular fill material forming co-joined assembly.
 53. A method of placing modular fill material forming co-joined assemblies as described in claim 52, wherein said reinforcement member comprises a steel reinforcement bar.
 54. A method of placing modular fill material forming co-joined assemblies as described in claim 52, wherein said step of placing said at least one reinforcement member comprises the step of horizontally inserting said reinforcement member into said space of at least one said fill material form.
 55. A method of placing modular fill material forming co-joined assemblies as described in claim 52, wherein said step of placing said at least one reinforcement member comprises the step of vertically inserting said reinforcement member into said space of at least one said fill material form.
 56. A method of placing modular fill material forming co-joined assemblies as described in claim 52, wherein said step of placing said at least one reinforcement member comprises the step of placing said at least one reinforcement member in a horizontal orientation within said space of at least one said fill material form.
 57. A method of placing modular fill material forming co-joined assemblies as described in claim 52, wherein said step of placing said at least one reinforcement member comprises the step of placing said at least one reinforcement member in a vertical orientation within said space of at least one said fill material form.
 58. A method of placing modular fill material forming co-joined assemblies as described in claim 52, wherein said step of placing said at least one reinforcement member comprises the step of joining said reinforcement member to at least one said connection element.
 59. A method of placing modular fill material forming co-joined assemblies as described in claim 58, wherein said step of joining said reinforcement member to at least one said connection element comprises the step of tying down said reinforcement member to said connection element.
 60. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein at least one said forming panel comprises an insulating forming panel.
 61. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein at least one said forming panel comprises a forming panel made of a material selected from the group consisting of wood, fiber, polymer, expanded polystyrene, extruded polystyrene, steel, metal alloy, epoxy, or plastic composite.
 62. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said connection element comprises a rigid tie.
 63. A method of placing modular fill material forming co-joined assemblies as described in claim 62, wherein said rigid tie comprises a rigid tie adapted to be joined to at least one reinforcement member.
 64. A method of placing modular fill material forming co-joined assemblies as described in claim 62, wherein said rigid tie further comprises a rigid tie having at least one cradle adapted to hold at least one reinforcement member.
 65. A method of placing modular fill material forming co-joined assemblies as described in claim 62, wherein said rigid tie maintains a separation distance of said first forming panel and said second forming panel.
 66. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said connection element comprises a flexible tie.
 67. A method of placing modular fill material forming co-joined assemblies as described in claim 66, wherein said flexible tie comprises a flexible tie adapted to permit at least one said fill material form to be collapsed.
 68. A method of placing modular fill material forming co-joined assemblies as described in claim 67, further comprising the step of collapsing said fill material form.
 69. A method of placing modular fill material forming co-joined assemblies as described in claim 68, wherein said step of collapsing comprises the step of substantially eliminating said space formed between said first forming panel and said second forming panel.
 70. A method of placing modular fill material forming co-joined assemblies as described in claim 66, wherein said flexible tie comprises a flexible tie selected from the group consisting of a folding tie, a pivot tie, an elastic tie, a wire tie, a monofilament tie, a frictional surface tie, or a flexible mesh tie.
 71. A method of placing modular fill material forming co-joined assemblies as described in claim 66, wherein said flexible tie comprises a flexible tie adapted to be joined to at least one reinforcement member.
 72. A method of placing modular fill material forming co-joined assemblies as described in claim 71, wherein said flexible tie adapted to be joined to at least one reinforcement member comprises a flexible tie spread to induce tension in said flexible tie.
 73. A method of placing modular fill material forming co-joined assemblies as described in claim 66, wherein said flexible tie maintains a separation distance of said first forming panel and said second forming panel.
 74. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said step of joining occurs at a remote location.
 75. A method of placing modular fill material forming co-joined assemblies as described in claim 74, wherein said remote location comprises a factory site.
 76. A method of placing modular fill material forming co-joined assemblies as described in claim 74, further comprising the step of transporting said modular fill material forming co-joined assembly to said ground location.
 77. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said first fill material form has a first edge and a second edge and wherein said second fill material form has a third edge and a fourth edge, and wherein said step of joining comprises joining a first rail to said first edge and said third edge and joining a second rail to said second edge and said fourth edge.
 78. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said first fill material form has a first edge and a second edge and wherein said second fill material form has a third edge and a fourth edge, and wherein said step of joining comprises joining a first clip to said first edge and said third edge and joining a second clip to said second edge and said fourth edge.
 79. A method of placing modular fill material forming co-joined assemblies as described in claim 40, further comprising the step of forming a cavity in said modular fill material forming co-joined assembly defined by communication of each said space of each said fill material form.
 80. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said ground location comprises a building site.
 81. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said centroid is a mass centroid.
 82. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said centroid is an area centroid.
 83. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said lift securement element comprises a lift securement element selected from the group consisting of a hook, clasp, ring, frictional surface, weld, tie, strap, mechanical fastener, or connector.
 84. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said lift securement element comprises a reinforcement member placed within at least one said space.
 85. A method of placing modular fill material forming co-joined assemblies as described in claim 84, wherein said reinforcement member comprises a reinforcement member adapted for connection to said lift attachment element.
 86. A method of placing modular fill material forming co-joined assemblies as described in claim 84, wherein said reinforcement member comprises a horizontal reinforcement member.
 87. A method of placing modular fill material forming co-joined assemblies as described in claim 84, wherein said reinforcement member comprises a vertical reinforcement member.
 88. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said step of positioning comprises symmetrically arranging said at least one lift securement element about said axis of lift for said centroid.
 89. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said aerial conveyance device comprises an aerial conveyance device selected from the group consisting of a crane, elevator, lift, pulley system, aircraft, or lifting system.
 90. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said lift attachment element comprises a lift attachment element selected from the group consisting of a hook, clasp, ring, tong, frictional surface, weld, tie, strap, mechanical fastener, or connector.
 91. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said lift attachment element is adapted for connection to a reinforcement member.
 92. A method of placing modular fill material forming co-joined assemblies as described in claim 40, wherein said placement location comprises a fill material pour site.
 93. A method of placing modular fill material forming co-joined assemblies as described in claim 92, wherein said fill material pour site comprises a high-rise fill material pour site.
 94. A method of placing modular fill material forming co-joined assemblies as described in claim 40, further comprising the step of establishing a securement integrity system to fortify a structural integrity of said modular fill material forming co-joined assembly during said step of transporting said modular fill material forming co-joined assembly.
 95. A method of placing modular fill material forming co-joined assemblies as described in claim 94, wherein said securement integrity system comprises at least one strengthening element established on said modular fill material forming co-joined assembly.
 96. A method of placing modular fill material forming co-joined assemblies as described in claim 95, wherein said strengthening element comprises a high-strength fastener joining said lift securement element to said modular fill material forming co-joined assembly.
 97. A modular fill material forming co-joined assembly placement system, comprising: a first forming panel; a second forming panel; a fill material form having at least one connection element joined to at least said first forming panel and at least said second forming panel; a space within said fill material form between said first forming panel and said second forming panel; a modular fill material forming co-joined assembly having at least a first fill material form joined to at least a second fill material form; a centroid of said modular fill material forming co-joined assembly; an axis of lift for said centroid of said modular fill material forming co-joined assembly; at least one lift securement element established on said modular fill material forming co-joined assembly adapted to be positioned to correlate with said axis of lift for said centroid of said modular fill material forming co-joined assembly. 98-137. (Cancelled)
 138. A method of placing modular fill material forming co-joined assemblies as described in claim 40, further comprising the step of affixing a brace attachment element joined to said modular fill material forming co-joined assembly in a continuously repositionable location.
 139. A method of placing modular fill material forming co-joined assemblies as described in claim 138, further comprising permanently joining said brace attachment element to said modular fill material forming co-joined assembly.
 140. A method of placing modular fill material forming co-joined assemblies as described in claim 138, further comprising temporarily joining said brace attachment element to said modular fill material forming co-joined assembly.
 141. A method of placing modular fill material forming co-joined assemblies as described in claim 138, further comprising joining at least one exposed rail to said modular fill material forming co-joined assembly.
 142. A method of placing modular fill material forming co-joined assemblies as described in claim 141, further comprising slidingly engaging said brace attachment element to said exposed rail.
 143. A method of placing modular fill material forming co-joined assemblies as described in claim 142, further comprising securing said brace attachment element to said exposed rail with a screw.
 144. A method of placing modular fill material forming co-joined assemblies as described in claim 138, further comprising joining a brace to said brace attachment element.
 145. A method of placing modular fill material forming co-joined assemblies as described in claim 144, wherein said brace comprises a kicker.
 146. A method of placing modular fill material forming co-joined assemblies as described in claim 144, further comprising supporting said modular fill material forming co-joined assembly with said brace.
 147. A method of placing modular fill material forming co-joined assemblies as described in claim 144, further comprising the steps of anchoring said brace to an anchor location and continuously repositioning said brace attachment element to a desired location.
 148. A method of placing modular fill material forming co-joined assemblies as described in claim 147, wherein said desired location comprises a location of said brace attachment element corresponding to a plumb position of said modular fill material forming co-joined assembly.
 149. A method of placing modular fill material forming co-joined assemblies as described in claim 138, further comprising rapidly deploying said brace attachment element.
 150. A method of placing modular fill material forming co-joined assemblies as described in claim 149, wherein said step of rapidly deploying said brace attachment element comprises the step of deploying within a period of time selected from the group consisting of about 90 seconds, about 2 minutes, about 3 minutes, about 5 minutes, or about 10 minutes.
 151. A method of placing modular fill material forming co-joined assemblies as described in claim 149, wherein said step of rapidly deploying said brace attachment element further comprises the step of affixing said brace attachment element in a continuously repositionable location with a screw.
 152. A modular fill material forming co-joined assembly placement system as described in claim 97, further comprising a brace attachment element affixed in a continuously repositionable location joined to said modular fill material forming co-joined assembly. 153-165. (Cancelled)
 166. A method of placing modular fill material forming co-joined assemblies as described in claim 40, further comprising the steps of: establishing an enclosure location having an outside enclosure boundary, an enclosure space, and an inside enclosure boundary; transporting an outer enclosure forming panel to said enclosure location; transporting at least one enclosure reinforcement member to said enclosure location; transporting an inner enclosure forming panel to said enclosure location; orienting said outer enclosure forming panel to substantially coincide with said outside enclosure boundary; positioning said outer enclosure forming panel substantially at said outside enclosure boundary; orienting said at least one enclosure reinforcement member to fit within said enclosure space; placing said at least one enclosure reinforcement member within said enclosure space after said step of positioning said outer enclosure forming panel; orienting said inner enclosure forming panel to substantially coincide with said inside enclosure boundary; positioning said inner enclosure forming panel substantially at said inside enclosure boundary after said step of placing said at least one enclosure reinforcement member; joining at least one enclosure connection element to said outer enclosure forming panel and said inner enclosure forming panel.
 167. A method of placing modular fill material forming co-joined assemblies as described in claim 166, further comprising the step of establishing at least one lift securement element on said outer enclosure forming panel.
 168. A method of placing modular fill material forming co-joined assemblies as described in claim 167, wherein said step of transporting said outer enclosure forming panel comprises the step of connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said outer enclosure forming panel.
 169. A method of placing modular fill material forming co-joined assemblies as described in claim 167, wherein said step of positioning said outer enclosure forming panel comprises the step of positioning said outer enclosure forming panel while said lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said outer enclosure forming panel.
 170. A method of placing modular fill material forming co-joined assemblies as described in claim 166, further comprising the step of establishing at least one lift securement element on said enclosure reinforcement member.
 171. A method of placing modular fill material forming co-joined assemblies as described in claim 170, wherein said step of transporting said enclosure reinforcement member comprises the step of connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said enclosure reinforcement member.
 172. A method of placing modular fill material forming co-joined assemblies as described in claim 170, wherein said step of positioning said enclosure reinforcement member comprises the step of positioning said enclosure reinforcement member while said lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said enclosure reinforcement member.
 173. A method of placing modular fill material forming co-joined assemblies as described in claim 166, further comprising the step of establishing at least one lift securement element on said inner enclosure forming panel.
 174. A method of placing modular fill material forming co-joined assemblies as described in claim 173, wherein said step of transporting said inner enclosure forming panel comprises the step of connecting said at least one lift attachment element of said aerial conveyance device to said at least one lift securement element of said inner enclosure forming panel.
 175. A method of placing modular fill material forming co-joined assemblies as described in claim 173, wherein said step of positioning said inner enclosure forming panel comprises the step of positioning said inner enclosure forming panel while said lift attachment element of said aerial conveyance device is connected to said at least one lift securement element of said inner enclosure forming panel.
 176. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said steps of establishing an enclosure location, transporting an outer enclosure forming panel, transporting at least one enclosure reinforcement member, transporting an inner enclosure forming panel, orienting said outer enclosure forming panel, positioning said outer enclosure forming panel, orienting said at least one enclosure reinforcement member, placing said at least one enclosure reinforcement member, orienting said inner enclosure forming panel, positioning said inner enclosure forming panel, and joining at least one enclosure connection element to said outer enclosure forming panel occur after said step of placing said modular fill material forming co-joined assembly.
 177. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said enclosure location comprises a corner opening.
 178. A method of placing modular fill material forming co-joined assemblies as described in claim 177, wherein said corner opening comprises a corner opening having a width selected from the group consisting of about 1 foot, about 2 feet, about 5 feet, or about 15 feet.
 179. A method of placing modular fill material forming co-joined assemblies as described in claim 177, further comprising placing at least one fill material form adjacent to said corner opening.
 180. A method of placing modular fill material forming co-joined assemblies as described in claim 179, further comprising joining said outer enclosure forming panel to an outer forming panel of said fill material form.
 181. A method of placing modular fill material forming co-joined assemblies as described in claim 179, further comprising joining said inner enclosure forming panel to an inner forming panel of said fill material form.
 182. A method of placing modular fill material forming co-joined assemblies as described in claim 179, further comprising placing at least one reinforcement member within said space of said fill material form.
 183. A method of placing modular fill material forming co-joined assemblies as described in claim 182, further comprising joining said enclosure reinforcement member to said reinforcement member placed within said space of said fill material form.
 184. A method of placing modular fill material forming co-joined assemblies as described in claim 183, wherein said step of joining said enclosure reinforcement member comprises tying down said enclosure reinforcement member to said reinforcement member placed within said space of said fill material form.
 185. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said enclosure location comprises an in-line opening.
 186. A method of placing modular fill material forming co-joined assemblies as described in claim 185, wherein said in-line opening comprises an in-line opening having a width selected from the group consisting of about 1 foot, about 2 feet, about 5 feet, or about 15 feet.
 187. A method of placing modular fill material forming co-joined assemblies as described in claim 185, further comprising placing at least one fill material form adjacent to said in-line opening.
 188. A method of placing modular fill material forming co-joined assemblies as described in claim 187, further comprising joining said outer enclosure forming panel to an outer forming panel of said fill material form.
 189. A method of placing modular fill material forming co-joined assemblies as described in claim 187, further comprising joining said inner enclosure forming panel to an inner forming panel of said fill material form.
 190. A method of placing modular fill material forming co-joined assemblies as described in claim 187, further comprising placing at least one reinforcement member within said space of said fill material form.
 191. A method of placing modular fill material forming co-joined assemblies as described in claim 190, further comprising joining said enclosure reinforcement member to said reinforcement member placed within said space of said fill material form.
 192. A method of placing modular fill material forming co-joined assemblies as described in claim 191, wherein said step of joining said enclosure reinforcement member comprises tying down said enclosure reinforcement member to said reinforcement member placed within said space of said fill material form.
 193. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said enclosure location comprises a fill material pour site.
 194. A method of placing modular fill material forming co-joined assemblies as described in claim 193, wherein said fill material pour site comprises a high-rise fill material pour site.
 195. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said enclosure reinforcement member comprises a steel reinforcement bar.
 196. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said step of placing at least one enclosure reinforcement member comprises the step of placing at least one enclosure reinforcement member in a horizontal orientation.
 197. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said step of placing at least one enclosure reinforcement member comprises the step of placing at least one enclosure reinforcement member in a vertical orientation.
 198. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said step of positioning said outer enclosure forming panel comprises the step of positioning said outer enclosure forming panel from an inside direction.
 199. A method of placing modular fill material forming co-joined assemblies as described in claim 166, wherein said outer enclosure forming panel is substantially braced by said inner enclosure forming panel.
 200. A modular fill material forming co-joined assembly placement system as described in claim 97, further comprising: an enclosure location having an outside enclosure boundary, an enclosure space, and an inside enclosure boundary; an outer enclosure forming panel oriented to substantially coincide with said outside enclosure boundary; said outer enclosure forming panel positioned substantially at said outside enclosure boundary; at least one enclosure reinforcement member oriented to fit within said enclosure space; said at least one enclosure reinforcement member placed within said enclosure space; an inner enclosure forming panel oriented to substantially coincide with said inside enclosure boundary; said inner enclosure forming panel positioned substantially at said inside enclosure boundary; at least one enclosure connection element joined to said outer enclosure forming panel and said inner enclosure forming panel; wherein said outer enclosure forming panel is substantially braced by said inner enclosure forming panel. 201-221. (Cancelled)
 222. A method of placing modular fill material forming co-joined assemblies as described in claim 40, further comprising the step of pouring a fill material into at least one said space after said step of placing said modular fill material forming co-joined assembly.
 223. A method of placing modular fill material forming co-joined assemblies as described in claim 222, wherein said fill material comprises concrete.
 224. A method of placing modular fill material forming co-joined assemblies as described in claim 222, further comprising creating a hardened form made of substantially said fill material.
 225. A method of placing modular fill material forming co-joined assemblies as described in claim 224, wherein said hardened form is a wall.
 226. A method of placing modular fill material forming co-joined assemblies as described in claim 224, further comprising creating a building structure having at least one said hardened form as a component.
 227. A method of placing modular fill material forming co-joined assemblies as described in claim 224, further comprising removing said modular fill forming structure from said hardened form.
 228. A modular fill material forming co-joined assembly placement system as described in claim 97, further comprising a fill material poured within at least said space of said fill material form. 229-232. (Cancelled) 